Method and system to increase electric brake clamping force accuracy
AssigneeHydro-Aire, Inc.
InventorsGary DeVlieg, John Gowan
Life of this patent
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AssigneeHydro-Aire, Inc.
InventorsGary DeVlieg, John Gowan
Estimating the term…
The method and system for increasing accuracy of clamping force of electric aircraft carbon brakes, once braking has been commenced, provides a first pair of electric brake actuators with a range of low brake clamping force responsive to low brake clamping force commands, and a second pair of electric brake actuators with a range of high brake clamping force responsive to high brake clamping force commands. The first pair of electric brake actuators is actuated to apply a minimum residual braking force once wheel braking is commenced, and the second pair of electric brake actuators is actuated only when the commanded braking force is in the high range of brake clamping force.
A method and system for increasing accuracy of clamping force of electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes for the plurality of wheels to reduce brake wear when the aircraft is taxiing, comprising the steps of:
A system for increasing accuracy of clamping force of electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes for the plurality of wheels to reduce brake wear when the aircraft is taxiing, the system comprising:
A method and system for increasing accuracy of clamping force of electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes for the plurality of wheels to reduce brake wear when the aircraft is taxiing, comprising the steps of:
A system for increasing accuracy of clamping force of electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes for the plurality of wheels to reduce brake wear when the aircraft is taxiing, the system comprising:
Dependencies are inferred from the claim text.